EP2196391A3 - Structures de surface portante d'avion résistantes aux impacts et avion l'incluant - Google Patents

Structures de surface portante d'avion résistantes aux impacts et avion l'incluant Download PDF

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Publication number
EP2196391A3
EP2196391A3 EP09015475A EP09015475A EP2196391A3 EP 2196391 A3 EP2196391 A3 EP 2196391A3 EP 09015475 A EP09015475 A EP 09015475A EP 09015475 A EP09015475 A EP 09015475A EP 2196391 A3 EP2196391 A3 EP 2196391A3
Authority
EP
European Patent Office
Prior art keywords
leading edge
skin
structures
aircraft
reinforcement
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
EP09015475A
Other languages
German (de)
English (en)
Other versions
EP2196391B1 (fr
EP2196391A2 (fr
Inventor
Franco Olmi
Luiz Andre Romariz
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Embraer SA
Original Assignee
Embraer SA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Embraer SA filed Critical Embraer SA
Publication of EP2196391A2 publication Critical patent/EP2196391A2/fr
Publication of EP2196391A3 publication Critical patent/EP2196391A3/fr
Application granted granted Critical
Publication of EP2196391B1 publication Critical patent/EP2196391B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/28—Leading or trailing edges attached to primary structures, e.g. forming fixed slots

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Laminated Bodies (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Elimination Of Static Electricity (AREA)
  • Moulding By Coating Moulds (AREA)
EP09015475.8A 2008-12-15 2009-12-15 Structures de surface portante d'avion résistantes aux impacts et avion l'incluant Active EP2196391B1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12/335,524 US8123167B2 (en) 2008-12-15 2008-12-15 Impact resistant aircraft leading edge structures and aircraft including the same

Publications (3)

Publication Number Publication Date
EP2196391A2 EP2196391A2 (fr) 2010-06-16
EP2196391A3 true EP2196391A3 (fr) 2012-03-28
EP2196391B1 EP2196391B1 (fr) 2016-07-27

Family

ID=41694616

Family Applications (1)

Application Number Title Priority Date Filing Date
EP09015475.8A Active EP2196391B1 (fr) 2008-12-15 2009-12-15 Structures de surface portante d'avion résistantes aux impacts et avion l'incluant

Country Status (4)

Country Link
US (1) US8123167B2 (fr)
EP (1) EP2196391B1 (fr)
CN (1) CN101786499B (fr)
BR (1) BRPI0925220B1 (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FI20080208L (fi) 2008-03-13 2008-03-27 Patria Aerostructures Oy Ilma-aluksen johtoreunaelementti, menetelmä sen valmistamiseksi sekä siipi ja vakain
ITTO20080333A1 (it) * 2008-05-06 2009-11-07 Alenia Aeronautica Spa Bordo d'attacco per strutture alari ed impennaggi in termoplastico con struttura a doppio guscio irrigidita.
GB2471408B (en) * 2009-03-12 2011-03-09 Patria Aerostructures Oy Leading edge element of aircraft, method for manufacturing one, wing and stabilizer
DE102010036154B4 (de) * 2010-09-02 2017-01-26 Airbus Operations Gmbh Luft absaugende Fahrzeugrumpfkomponente, Verfahren zum Herstellen einer Luft absaugenden Fahrzeugrumpfkomponente und Fahrzeug, insbesondere Flugzeug, mit einer Luft absaugenden Fahrzeugrumpfkomponente
CN102390520B (zh) * 2011-09-29 2014-06-18 西北工业大学 一种能够提高飞机抗鸟撞性能的尾翼
GB201120707D0 (en) * 2011-12-01 2012-01-11 Airbus Operations Ltd Leading edge structure
US9708030B1 (en) 2011-12-08 2017-07-18 The Boeing Company Impact-energy tolerant method and structures
ES2421410B1 (es) * 2012-02-29 2014-10-28 Airbus Operations, S.L. Borde de salida de una superficie aerodinamica de una aeronave
FR2989666B1 (fr) * 2012-04-19 2014-12-05 Eurocopter France Surface aerodynamique portante d'aeronef, et aeronef muni de ladite surface aerodynamique portante
US8968437B2 (en) * 2012-05-02 2015-03-03 Michael J Kline Jet engine with deflector
ES2606245T3 (es) 2012-07-17 2017-03-23 Airbus Operations, S.L. Borde de ataque altamente integrado de una superficie sustentadora de una aeronave
FR2993857B1 (fr) * 2012-07-26 2015-03-27 Airbus Operations Sas Dispositif de protection d'une structure de longeron avant d'un caisson central d'aile d'aeronef et d'au moins un equipement situe dans ladite aile
EP2690008B1 (fr) * 2012-07-26 2015-06-10 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hélicoptère avec corps arrière aérodynamique et émoussé
FR2999344B1 (fr) * 2012-12-10 2018-04-13 Airbus Operations Antenne de radar meteorologique embarque pour aeronef et aeronef associe
EP2886449A1 (fr) 2013-12-23 2015-06-24 Airbus Operations S.L. Bord d'attaque pour surface de sustentation d'un aéronef
EP2962840A1 (fr) * 2014-06-30 2016-01-06 Airbus Operations, S.L. Bord d'attaque pour surface portante d'aéronef et son procédé de fabrication
JP6782533B2 (ja) * 2015-08-26 2020-11-11 三菱航空機株式会社 航空機の前縁構造体、航空機の翼及び航空機
ES2740623T3 (es) 2016-03-14 2020-02-06 Airbus Operations Sl Procedimiento y herramienta de moldeo por inyección para fabricar una sección de borde de ataque con control de flujo laminar híbrido para una aeronave
CN107434031A (zh) 2016-05-25 2017-12-05 空中客车简化股份公司 飞行器翼体的结构部件和包括该结构部件的飞行器
EP3335986B1 (fr) * 2016-12-19 2019-11-20 Airbus Operations S.L. Dérive dorsale antichoc
US10556701B2 (en) * 2017-04-14 2020-02-11 Rohr, Inc. Bird-strike energy absorbing net
US11454121B2 (en) * 2018-09-28 2022-09-27 General Electric Company Airfoil with leading edge guard
US11518502B2 (en) * 2019-04-30 2022-12-06 Textron Innovations Inc. Energy absorption stabilizers and methods
CN112249300B (zh) * 2020-10-22 2022-02-15 航天特种材料及工艺技术研究所 一种碳纤维复合材料翼面前缘结构
US11725524B2 (en) 2021-03-26 2023-08-15 General Electric Company Engine airfoil metal edge
CN113772108B (zh) * 2021-09-15 2023-08-04 中国航空工业集团公司西安飞机设计研究所 一种尾翼前缘分鸟器结构
US11988103B2 (en) 2021-10-27 2024-05-21 General Electric Company Airfoils for a fan section of a turbine engine
US11655828B2 (en) 2021-10-27 2023-05-23 General Electric Company Anti-icing systems and airfoils for a fan section of a turbine engine
US11767607B1 (en) 2022-07-13 2023-09-26 General Electric Company Method of depositing a metal layer on a component

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6279228B1 (en) * 1997-07-24 2001-08-28 Fuji Jukogyo Kabushiki Kaisha Method of making a leading edge structure of aircraft airfoil
US20070138340A1 (en) * 2003-08-27 2007-06-21 Arafat Husam R Protective skin for aircraft
WO2007071398A1 (fr) * 2005-12-20 2007-06-28 Airbus Deutschland Gmbh Dispositif de protection
GB2440133A (en) * 2006-07-18 2008-01-23 Gkn Aerospace Transparency Sys A de-icing heated leading edge component of an aircraft
WO2008109763A2 (fr) * 2007-03-06 2008-09-12 The Boeing Company Panneau élastique pour avion

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2381662A1 (fr) * 1977-02-28 1978-09-22 Aerospatiale Pale, notamment pour un rotor d'helicoptere, et son procede de fabrication
US4485991A (en) * 1983-07-01 1984-12-04 Fuller Brian L Rollable airfoil
US4657615A (en) * 1984-08-20 1987-04-14 The Boeing Company Composite leading edge/spar member for an aircraft control surface
EP1910863B1 (fr) 2005-07-14 2014-03-26 TELEFONAKTIEBOLAGET LM ERICSSON (publ) Adaptation d'ensemble de modeles par diffusion de masse de probabilite
EP1764307A1 (fr) * 2005-09-14 2007-03-21 EADS Construcciones Aeronauticas, S.A. Procédé de fabrication d'un bord d'attaque monolithique
ES2329324B1 (es) * 2007-03-30 2010-09-06 Airbus España, S.L. Borde de ataque de aeronave de material compuesto reforzado.
US7857588B2 (en) * 2007-07-06 2010-12-28 United Technologies Corporation Reinforced airfoils

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6279228B1 (en) * 1997-07-24 2001-08-28 Fuji Jukogyo Kabushiki Kaisha Method of making a leading edge structure of aircraft airfoil
US20070138340A1 (en) * 2003-08-27 2007-06-21 Arafat Husam R Protective skin for aircraft
WO2007071398A1 (fr) * 2005-12-20 2007-06-28 Airbus Deutschland Gmbh Dispositif de protection
GB2440133A (en) * 2006-07-18 2008-01-23 Gkn Aerospace Transparency Sys A de-icing heated leading edge component of an aircraft
WO2008109763A2 (fr) * 2007-03-06 2008-09-12 The Boeing Company Panneau élastique pour avion

Also Published As

Publication number Publication date
BRPI0925220B1 (pt) 2020-07-21
EP2196391B1 (fr) 2016-07-27
US8123167B2 (en) 2012-02-28
BRPI0925220A2 (pt) 2017-02-14
EP2196391A2 (fr) 2010-06-16
US20100148006A1 (en) 2010-06-17
CN101786499A (zh) 2010-07-28
CN101786499B (zh) 2014-11-26

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